# Service difficulty reports: N815AT, cancelled May 17, 2006

A list on [N815AT, cancelled May 17, 2006](https://openairdocs.org/deregistered/N815AT-2006-05-17.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR AT9900800](https://openairdocs.org/sdr/AT9900800.md): Emergency Lights · intermittent · Nov 8, 1999 · N815AT · Doug DC932 · Emergency Lighting
  > WITH EMERGENCY EXIT LIGHTS SELECTED OFF AND BATTERY SWITCH OFF. THE OVERWING EXIT LIGHTS REMAIN ILLUMINATED WITH SWITCH (BATT) ON ALL EMERGENCY EVAC LIGHTS ARE OUT/OFF. POWERED DOWN AIRCRAFT, THE REPOWERED EMERGENCY LIGHTS CHECKED NORMAL IAW DC9 MM 33-53.
- [SDR AT9900641](https://openairdocs.org/sdr/AT9900641.md): Skin · corroded · Sep 10, 1999 · N815AT · Doug DC932 · Fuselage Main, Plate/Skin
  > DURING RAMP OPERATIONS, CORROSION WAS FOUND ON THE FUSELAGE SKIN AT BS 574 BETWEEN LONGERONS 29L AND 29R. THE AREA HAS AN EXISTING SKIN CUTOUT AND AN EXTERNAL DOUBLER. CRACKS WERE ALSO FOUND ON 2 LONGERONS. THE DAMAGED SKIN AND EXISTING REPAIR WERE REMOVED.
- [SDR AT9900498](https://openairdocs.org/sdr/AT9900498.md): Frame · cracked · Jul 12, 1999 · N815AT · Doug DC932 · Fuselage Main, Frame
  > FOUND THE TAIL SECTION CANTED FRAME AT BS 1143 RIGHT SIDE CRACKED AT REAR STAIR ACTUATOR MOUNT. FABRICATED REPAIR DOUBLERS, HEAT TREAT ANGLES, DRILLED, DEBURRED, AND INSTALLED IAW DC9 SRM 51-10-2A, 51-30-2, 51-10-4, 51-10-3, AND TIMCO RES NR 07025 AND TIMCO E
- [SDR AT9900364](https://openairdocs.org/sdr/AT9900364.md): Battery Charger · defective · May 6, 1999 · N815AT · Doug DC932 · Emergency Lighting
  > FOUND THE AFT SECTION OF THE EMERGENCY FLOOR PATH LIGHTING INOPERATIVE. REPACED BATTERY CHARGER IAW MM 33-54-0, OPS CHECKED GOOD.
- [SDR AT9900182](https://openairdocs.org/sdr/AT9900182.md): Lever · out of adjust · Mar 9, 1999 · N815AT · Doug DC932 · Landing Gear Selector
  > ON CLIMB, GEAR LEVER WILL NOT RAISE, AIR RETURN. RIGGED LANDING GEAR CONTROL LEVEL ANTI-RETRACTION LATCH IAW DC9 MM 32-31-1. CHECKED RIG ON GROUND SENSE CONTROL, MECHANICAL RIG CHECK GOOD IAW DC9 MM 32-23-1.
- [SDR AT9900214](https://openairdocs.org/sdr/AT9900214.md): Thrust Reverser · chafed · Mar 3, 1999 · N815AT · Doug DC932 · Engine Thrust Reverser
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND ON THE NR 1 ENGINE THRUST REVERSER AT THE FORWARD MATING FLANGE TO THE ENGINE COWLING WITH A CHAFED AREA APPROXIMATELY FIVE INCHES LONG THRU THE BASE OF THE METAL. CUT OUT CHAFED AREA, FABRICATED, FORM FILLER AND
- [SDR AT9900180](https://openairdocs.org/sdr/AT9900180.md): Angle · cracked · Mar 3, 1999 · N815AT · Doug DC932 · Fuselage Miscellaneous Structure
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND A CRACK IN VERTICAL LEG OF NR 2 PYLON UPPER ATTACH ANGLE AT BS 980. STOP DRILLED CRACK, HIGH FREQUENCT EDDY CURRENT VERIFIED CRACK WAS STOP, FABRICATED AND INSTALLED REPAIR IAW DC9 SRM 51-30-2, AND RES NR 99442.
- [SDR AT9900213](https://openairdocs.org/sdr/AT9900213.md): Fitting · chafed · Feb 23, 1999 · N815AT · Doug DC932 · Landing Gear Door Actuator
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE LEFT HAND MAIN LANDING GEAR DOOR ACTUATOR FITTING IN WHEEL WELL WITH A DEEP CHAFE MARK FROM A HYDRAULIC LINE RUBBING AT BS 699. BLEND AREA SMOOTH, HFEC VERIFY NO CRACKS NOTED. RESTORED ORIGINAL FINISHED, ALOD
- [SDR AT9900193](https://openairdocs.org/sdr/AT9900193.md): Support · corroded · Feb 19, 1999 · N815AT · Doug DC932 · Fuselage Miscellaneous Structure
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FLOOR SUPPORT IN THE FORWARD CARGO PIT AT BS 238 OVER L-28R CORRODED. REMOVED FLOOR SUPPORT AND FABRICATED REPAIR, ALODINE, PRIMED, AND INSTALLED SUPPORT AND REPAIR IAW DC9 SRM 53-01-FIG 1, 51-10-3, AND 51-30-
- [SDR AT9900167](https://openairdocs.org/sdr/AT9900167.md): Bracket · corroded · Feb 15, 1999 · N815AT · Doug DC932 · Cargo/Baggage Doors
  > SCHEDULED INSPECTION AT AERO CORP, FL, FOUND A CORRODED ANGLE BRACKET ON FORWARD LOWER CARGO DOOR. REMOVED L ANGLE BRACKET, FABRICATED NEW ANGLE, REPAIR DOUBLER AND INSTALLED IAW DC9 SRM 53-05 FIG 7 PAGE 8.
- [SDR AT9900212](https://openairdocs.org/sdr/AT9900212.md): Bulkhead Bracket · corroded · Feb 12, 1999 · N815AT · Doug DC932 · Fuselage Main, Bulkhead
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE CANTED BULKHEAD LEFT HAND LOWER ATTACH BRACKETS HAVE CORROSION RUNNING UNDER THEM AT LONGERON 11 ON THE BACK OF FRAME AT BS 1180. REMOVED BRACKETS AND CORROSION, CUT OUT AREA, FABRICATED FRAME REPAIR AND DOUBL
- [SDR AT9900199](https://openairdocs.org/sdr/AT9900199.md): Frame · cracked · Feb 12, 1999 · N815AT · Doug DC932 · Fuselage Main, Frame
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT PIT LEFT HAND FLOOR SUPPORT FRAME CRACKED AT BS 870. REMOVED CRACKED FRAME, REPAIR FRAME IAW DC9 EA NR 12-5321-29-C1362 AND REINSTALLED FLOOR SUPPORT IAW DC9 SRM 51-30-2.
- [SDR AT9900198](https://openairdocs.org/sdr/AT9900198.md): Skin · dented · Feb 12, 1999 · N815AT · Doug DC932 · Fuselage Main, Plate/Skin
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND A DENT OUT OF LIMITS AT BS 195R. FABRICATED DOUBLER AND FINGER DOUBLER, DRILLED, DEBURRED, TREATED, PRIMED AND INSTALLED IAW DC9 SRM 51-30-2, 51-10-2, AND RES NR 99443.
- [SDR AT9900200](https://openairdocs.org/sdr/AT9900200.md): Frame · cracked · Feb 11, 1999 · N815AT · Doug DC932 · Fuselage Main, Frame
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE LEFT HAND LOWER FUSELAGE FRAME FITTING AT BS 692 CRACKED AT THE BOLT HOLE IN UPPER FLANGE IN FORWARD LOWER INBOARD CORNER OF LEFT WHEEL WELL. STOP DRILLED CRACK, VERIFY BY HFEC, FABRICATED REPAIR ANGLE, TREATE
- [SDR AT9900192](https://openairdocs.org/sdr/AT9900192.md): Skin · cracked · Feb 11, 1999 · N815AT · Doug DC932 · Fuselage Main, Plate/Skin
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND A CRACK ON SKIN LEFT HAND SIDE JUST BELOW L-14L AT BS 950. NDT MARKED ENDS OF CRACK, REMOVED CRACK, FABRICATED REPAIR DOUBLER, TREATED, PRIMED AND INSTALLED REPAIR IAW DC9 SRM 51-30-2, 53-04 FIG 3A, 51-10-3, AND R
- [SDR AT9900169](https://openairdocs.org/sdr/AT9900169.md): Strap · corroded · Feb 11, 1999 · N815AT · Doug DC932 · Fuselage Miscellaneous Structure
  > SCHEDULED INSPECTION AT AERO CORP, FL, FOUND SIDE WALL TRIM STRAP AT BS 427 RIGHT SIDE CORRODED. MECHANICALLY REMOVED CORROSION, FABRICATED STRAP, TREATED, PRIMED, AND INSTALLED IAW DC9 SRM 51-10-2, 51-10-3, AND 53-01 FIG 1.
- [SDR AT9900215](https://openairdocs.org/sdr/AT9900215.md): Angle · chafed · Feb 9, 1999 · N815AT · Doug DC932 · Passenger/Crew Doors
  > SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE L-1 DOOR STRIKING BEHIND MOUNT U-CHANNEL ANGLE ON AFT DOOR JAMB AT UPPER STOP BOLT. BLENDED OUT DAMAGE AREA TO HAVE MINIMUM RADIUS, TREATED TRIMMED AREA, PRIMED AND DRESSED UP IAW DC9 53-01-0, 53-11-0, AND RE
- [SDR AT9900168](https://openairdocs.org/sdr/AT9900168.md): Floor Track · corroded · Feb 9, 1999 · N815AT · Doug DC932 · Fuselage, Seat/Cargo Attach Fittings
  > SCHEDULED INSPECTION AT AERO CORP, FL, FOUND CARGO FLOOR TRACK AT BS 307-503 CORRODED. MECHANICALLY REMOVED CORROSION, REMOVED, REPLACED AND FABRICATED NEW TRACK SECTION, DRILLED, DEBURRED, ALODINED, PRIMED AND INSTALLED IAW DC9 SRM 51-10-4, 53-05 FIG 4C, AND
- [SDR AT9900205](https://openairdocs.org/sdr/AT9900205.md): Track · corroded · Feb 7, 1999 · N815AT · Doug DC932 · Fuselage, Seat/Cargo Attach Fittings
  > SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE FORWARD CARGO FLOOR TRACK AT BS 318 TO 370 RIGHT SIDE CORRODED. FABRICATED NEW SEAT TRACK, DRILLED, DEBURRED, ALODINED, PRIMED, AND INSTALLED IAW DC9 SRM 53-10-3, 51-10-4, AND 51-10-3.
- [SDR AT9900204](https://openairdocs.org/sdr/AT9900204.md): Track · corroded · Feb 7, 1999 · N815AT · Doug DC932 · Fuselage, Seat/Cargo Attach Fittings
  > SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE FORWARD CARGO DOOR TRACK AT BS 351 TO 370 LEFT HAND SIDE CORRODED. REMOVED CORROSION, LOCATED AND DRILLED NEW TRACK IAW DC9 SRM 53-10-3, 51-10-3, AND 53-20-0.
- [SDR AT9900203](https://openairdocs.org/sdr/AT9900203.md): Track · corroded · Feb 7, 1999 · N815AT · Doug DC932 · Fuselage, Seat/Cargo Attach Fittings
  > SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE FORWARD CARGO FLOOR TRACK AT BS 427 TO 503 CORRODED. REMOVED CORROSION, FABRICATED, DRILLED, DEBURRED, AND INSTALLED NEW SEAT TRACK IAW DC9 SRM 53-05 FIG 4C, 51-10-3, AND 51-10-4.
- [SDR AT9900202](https://openairdocs.org/sdr/AT9900202.md): Track · corroded · Feb 7, 1999 · N815AT · Doug DC932 · Fuselage, Seat/Cargo Attach Fittings
  > SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE FORWARD CARGO FLOOR TRACK CORRODED AT BS 389 TO 465. FABRICATED, DRILLED, DEBURRED, AND INSTALLED NEW SEAT TRACK IAW DC9 SRM 53-05 FIG 4C, 51-10-3 AND 51-10-4.

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N815AT' AND deregistration_id = 'N815AT-2006-05-17'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N815AT-2006-05-17/reports

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